RU2011125301A - METHOD FOR PRODUCING MICROMECHANICAL COMPONENT - Google Patents

METHOD FOR PRODUCING MICROMECHANICAL COMPONENT Download PDF

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Publication number
RU2011125301A
RU2011125301A RU2011125301/28A RU2011125301A RU2011125301A RU 2011125301 A RU2011125301 A RU 2011125301A RU 2011125301/28 A RU2011125301/28 A RU 2011125301/28A RU 2011125301 A RU2011125301 A RU 2011125301A RU 2011125301 A RU2011125301 A RU 2011125301A
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RU
Russia
Prior art keywords
plates
specified
support
plate
component
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RU2011125301/28A
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Russian (ru)
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RU2498382C2 (en
Inventor
Александр ФЮССИНГЕР
Марко ВЕРАРДО
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Ниварокс-Фар С.А.
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Publication of RU2011125301A publication Critical patent/RU2011125301A/en
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Publication of RU2498382C2 publication Critical patent/RU2498382C2/en

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Classifications

    • G—PHYSICS
    • G04—HOROLOGY
    • G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B13/00—Gearwork
    • G04B13/02—Wheels; Pinions; Spindles; Pivots
    • G—PHYSICS
    • G04—HOROLOGY
    • G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B15/00—Escapements
    • G04B15/14—Component parts or constructional details, e.g. construction of the lever or the escape wheel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B81—MICROSTRUCTURAL TECHNOLOGY
    • B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
    • B81C3/00—Assembling of devices or systems from individually processed components
    • B81C3/002—Aligning microparts
    • B81C3/005—Passive alignment, i.e. without a detection of the position of the elements or using only structural arrangements or thermodynamic forces
    • G—PHYSICS
    • G04—HOROLOGY
    • G04B—MECHANICALLY-DRIVEN CLOCKS OR WATCHES; MECHANICAL PARTS OF CLOCKS OR WATCHES IN GENERAL; TIME PIECES USING THE POSITION OF THE SUN, MOON OR STARS
    • G04B13/00—Gearwork
    • G04B13/02—Wheels; Pinions; Spindles; Pivots
    • G04B13/027—Wheels; Pinions; Spindles; Pivots planar toothing: shape and design
    • G—PHYSICS
    • G04—HOROLOGY
    • G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00—Watchmakers' or watch-repairers' machines or tools for working materials
    • G—PHYSICS
    • G04—HOROLOGY
    • G04D—APPARATUS OR TOOLS SPECIALLY DESIGNED FOR MAKING OR MAINTAINING CLOCKS OR WATCHES
    • G04D3/00—Watchmakers' or watch-repairers' machines or tools for working materials
    • G04D3/0002—Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe
    • G04D3/0028—Watchmakers' or watch-repairers' machines or tools for working materials for mechanical working other than with a lathe for components of the escape mechanism
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B81—MICROSTRUCTURAL TECHNOLOGY
    • B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
    • B81C2203/00—Forming microstructural systems
    • B81C2203/03—Bonding two components
    • B81C2203/038—Bonding techniques not provided for in B81C2203/031 - B81C2203/037
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B81—MICROSTRUCTURAL TECHNOLOGY
    • B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
    • B81C2203/00—Forming microstructural systems
    • B81C2203/05—Aligning components to be assembled
    • B81C2203/052—Passive alignment, i.e. using only structural arrangements or thermodynamic forces without an internal or external apparatus
    • B81C2203/054—Passive alignment, i.e. using only structural arrangements or thermodynamic forces without an internal or external apparatus using structural alignment aids, e.g. spacers, interposers, male/female parts, rods or balls
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49579—Watch or clock making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49799—Providing transitory integral holding or handling portion
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • Y10T29/49901—Sequentially associating parts on stationary aligning means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener

Abstract

1. Способ (1) изготовления микромеханического компонента (31, 41, 51), который включает следующие этапы:а) формирование (3), по меньшей мере, двух пластин (11, 13), каждая из которых включает рамку (15, 17), соединенную, по меньшей мере, одной перемычкой (12, 14) материала с деталью (19, 21) указанного компонента;отличающийся тем, что он также включает следующие этапы:б) установки (5) указанных, по меньшей мере, двух пластин на опору (23) таким образом, что указанные, по меньшей мере, две пластины располагаются одна поверх другой;в) закрепления (7) штифта (29) в отверстии (16, 18) указанных, по меньшей мере, двух установленных деталей для формирования компонента (31, 41, 51) таким образом, что одиночный штырь выступает, по меньшей мере, из одной из установленных пластин и может использоваться в качестве захватывающего средства;г) отделения (9) указанного сформированного компонента (31, 41, 51) от указанных, по меньшей мере, двух пластин (11, 13).2. Способ (1) по п.1, отличающийся тем, что этап б) включает следующие этапы для каждой пластины (11, 13):д) направление (B) указанной пластины при помощи установочных средств (25) для точной ориентации указанной пластины относительно опоры (23);е) скольжение (A) указанной пластины, по меньшей мере, по одной оси (22), закрепленной на опоре (23) до упора в заплечик (24) указанно оси для точной установки указанной пластины относительно опоры (23).3. Способ (1) по п.2, отличающийся тем, что каждое из указанных установочных средств включает, по меньшей мере, одно коническое кольцо, которое установлено на продолжении указанной, по меньшей мере, одной оси опоры (23) и которое взаимодействует с углублением (20, 26), выполненном в каждой из указанных, по меньшей м1. A method (1) for manufacturing a micromechanical component (31, 41, 51), which includes the following steps: a) forming (3) at least two plates (11, 13), each of which includes a frame (15, 17 ), connected by at least one jumper (12, 14) of the material with a part (19, 21) of the specified component; characterized in that it also includes the following steps: b) installation (5) of the indicated at least two plates on the support (23) in such a way that said at least two plates are located one on top of the other; c) securing the pin (7) of the pin (29) in the hole (16 , 18) the specified at least two installed parts for forming the component (31, 41, 51) so that a single pin protrudes from at least one of the installed plates and can be used as a gripping means; g) separation (9) said formed component (31, 41, 51) from said at least two plates (11, 13) .2. Method (1) according to claim 1, characterized in that step b) includes the following steps for each plate (11, 13): e) direction (B) of said plate using installation tools (25) for the exact orientation of said plate relative to the support (23); e) sliding (A) of said plate with at least one axis (22) fixed to a support (23) against the shoulder (24) of the indicated axis to precisely set said plate relative to the support (23). 3. The method (1) according to claim 2, characterized in that each of these installation means includes at least one conical ring, which is installed on the continuation of the specified at least one axis of the support (23) and which interacts with the recess ( 20, 26) performed in each of the indicated at least m

Claims (14)

1. Способ (1) изготовления микромеханического компонента (31, 41, 51), который включает следующие этапы:1. The method (1) of manufacturing a micromechanical component (31, 41, 51), which includes the following steps: а) формирование (3), по меньшей мере, двух пластин (11, 13), каждая из которых включает рамку (15, 17), соединенную, по меньшей мере, одной перемычкой (12, 14) материала с деталью (19, 21) указанного компонента;a) the formation (3) of at least two plates (11, 13), each of which includes a frame (15, 17) connected by at least one jumper (12, 14) of the material to the part (19, 21 ) the specified component; отличающийся тем, что он также включает следующие этапы:characterized in that it also includes the following steps: б) установки (5) указанных, по меньшей мере, двух пластин на опору (23) таким образом, что указанные, по меньшей мере, две пластины располагаются одна поверх другой;b) installation (5) of said at least two plates on a support (23) in such a way that said at least two plates are located one on top of the other; в) закрепления (7) штифта (29) в отверстии (16, 18) указанных, по меньшей мере, двух установленных деталей для формирования компонента (31, 41, 51) таким образом, что одиночный штырь выступает, по меньшей мере, из одной из установленных пластин и может использоваться в качестве захватывающего средства;c) fixing (7) the pin (29) in the hole (16, 18) of said at least two installed parts to form the component (31, 41, 51) so that a single pin protrudes from at least one from installed plates and can be used as an exciting tool; г) отделения (9) указанного сформированного компонента (31, 41, 51) от указанных, по меньшей мере, двух пластин (11, 13).d) separating (9) said formed component (31, 41, 51) from said at least two plates (11, 13). 2. Способ (1) по п.1, отличающийся тем, что этап б) включает следующие этапы для каждой пластины (11, 13):2. The method (1) according to claim 1, characterized in that step b) includes the following steps for each plate (11, 13): д) направление (B) указанной пластины при помощи установочных средств (25) для точной ориентации указанной пластины относительно опоры (23);d) the direction (B) of the specified plate using installation tools (25) for the exact orientation of the specified plate relative to the support (23); е) скольжение (A) указанной пластины, по меньшей мере, по одной оси (22), закрепленной на опоре (23) до упора в заплечик (24) указанно оси для точной установки указанной пластины относительно опоры (23).e) the sliding (A) of the specified plate, at least one axis (22), mounted on the support (23) until it stops in the shoulder (24) of the specified axis for accurate installation of the specified plate relative to the support (23). 3. Способ (1) по п.2, отличающийся тем, что каждое из указанных установочных средств включает, по меньшей мере, одно коническое кольцо, которое установлено на продолжении указанной, по меньшей мере, одной оси опоры (23) и которое взаимодействует с углублением (20, 26), выполненном в каждой из указанных, по меньшей мере, двух пластин на этапе а).3. The method (1) according to claim 2, characterized in that each of these installation means includes at least one conical ring, which is installed on the continuation of the specified at least one axis of the support (23) and which interacts with a recess (20, 26) made in each of said at least two plates in step a). 4. Способ (1) по п.2, отличающийся тем, что операция направления на этапе д) осуществляется с применением, по меньшей мере, двух установочных средств (25) для повышения точности указанного направления.4. The method (1) according to claim 2, characterized in that the direction operation in step d) is carried out using at least two installation means (25) to increase the accuracy of the specified direction. 5. Способ (1) по п.3, отличающийся тем, что каждое углубление (20, 26) выполнено в рамке (15, 17) указанных, по меньшей мере, двух пластин.5. The method (1) according to claim 3, characterized in that each recess (20, 26) is made in the frame (15, 17) of said at least two plates. 6. Способ (1) по п.3, отличающийся тем, что каждое углубление представляет собой пространство между рамкой (15, 17) и деталью (19, 21) каждой из указанных, по меньшей мере, двух пластин.6. The method (1) according to claim 3, characterized in that each recess represents the space between the frame (15, 17) and the part (19, 21) of each of the at least two plates. 7. Способ (1) по п.1, отличающийся тем, что каждая, по меньшей мере, одна перемычка (12, 14) материала включает узкое сечение у края, соединяемого с указанной деталью компонента для создания ослабленной зоны с целью упрощения этапа г).7. The method (1) according to claim 1, characterized in that each at least one jumper (12, 14) of the material includes a narrow section at the edge connected to the specified component part to create a weakened zone in order to simplify step d) . 8. Способ (1) по п.1, отличающийся тем, что на каждой пластине (11, 13) формируются несколько деталей (19, 21) для формирования нескольких компонентов (31, 41, 51) на этапе в).8. The method (1) according to claim 1, characterized in that on each plate (11, 13) several parts (19, 21) are formed to form several components (31, 41, 51) in step c). 9. Способ (1) по п.1, отличающийся тем, что штифт (29) продолжается с каждой стороны шкворневым хвостовиком, который включает шкворень для формирования шарнирной оси.9. The method (1) according to claim 1, characterized in that the pin (29) extends on each side with a pivot shank, which includes a pivot for forming a hinge axis. 10. Способ (1) по п.1, отличающийся тем, что штифт (29) имеет соосное кольцо (30), используемое в качестве упорного элемента для ограничения проникновения указанного штифта в указанные отверстия.10. The method (1) according to claim 1, characterized in that the pin (29) has a coaxial ring (30) used as a thrust element to limit the penetration of the specified pin into these holes. 11. Способ (1) по п.10, отличающийся тем, что указанное соосное кольцо (30) имеет зубья для формирования шестерни.11. The method (1) according to claim 10, characterized in that said coaxial ring (30) has teeth for forming a gear. 12. Способ (1) по п.1, отличающийся тем, что, по меньшей мере, одна из указанных пластин формируется на этапе а) при помощи процесса нанесения гальванического покрытия.12. The method (1) according to claim 1, characterized in that at least one of these plates is formed in step a) using a plating process. 13. Способ (1) по п.1, отличающийся тем, что, по меньшей мере, одна из указанных пластин формируется на этапе а) при помощи процесса микрообработки.13. The method (1) according to claim 1, characterized in that at least one of these plates is formed in step a) using a microprocessing process. 14. Способ (1) по п.1, отличающийся тем, что, по меньшей мере, один подэлемент устанавливается, по меньшей мере, на одну из указанных деталей в поперечном направлении относительно указанной пластины до, во время или после этапа б). 14. The method (1) according to claim 1, characterized in that at least one sub-element is mounted on at least one of these parts in the transverse direction relative to the specified plate before, during or after step b).
RU2011125301/28A 2008-11-21 2009-11-04 Method of making micromechanical component RU2498382C2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP08169687.4 2008-11-21
EP08169687A EP2189854A1 (en) 2008-11-21 2008-11-21 Method for manufacturing a micromechanical part
PCT/EP2009/064639 WO2010057777A1 (en) 2008-11-21 2009-11-04 Method for making a micromechanical part

Publications (2)

Publication Number Publication Date
RU2011125301A true RU2011125301A (en) 2012-12-27
RU2498382C2 RU2498382C2 (en) 2013-11-10

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US (1) US8661681B2 (en)
EP (2) EP2189854A1 (en)
JP (1) JP5548692B2 (en)
KR (1) KR20110086579A (en)
CN (1) CN102224464B (en)
HK (1) HK1163266A1 (en)
RU (1) RU2498382C2 (en)
TW (1) TWI520900B (en)
WO (1) WO2010057777A1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2400352A1 (en) 2010-06-22 2011-12-28 The Swatch Group Research and Development Ltd. Escapement system for a timepiece
CN103097965B (en) * 2010-07-19 2015-05-13 尼瓦洛克斯-法尔股份有限公司 Oscillating mechanism with elastic pivot and mobile for the transmission of energy
EP2794463B1 (en) * 2011-12-22 2017-03-15 CSEM Centre Suisse d'Electronique et de Microtechnique SA - Recherche et Développement Method for freeing a micromechanical part and a micromechanical part comprising sacrificial fasteners
CH706220B1 (en) * 2012-03-06 2022-05-31 Sigatec Sa Method for assembling a fragile component on a metal part and micromechanical part assembled according to this method.
US9151259B2 (en) * 2012-06-11 2015-10-06 Continental Automotive Systems, Inc. Stepped orifice hole
WO2014146842A1 (en) * 2013-03-22 2014-09-25 Omega Sa Unitary coaxial escapement anchor
EP2799939A1 (en) * 2013-04-30 2014-11-05 Universo S.A. Support for the treatment of micromechanical parts
EP3632839A1 (en) * 2013-12-20 2020-04-08 Rolex Sa Clock component
EP2942147B1 (en) * 2014-05-08 2018-11-21 Nivarox-FAR S.A. Clock escapement mechanism without lubrication
CH710543A2 (en) * 2014-12-19 2016-06-30 Omega Sa Process for producing a decorated element of a timepiece or jewelery, and element produced by the method.
EP3109199B1 (en) * 2015-06-25 2022-05-11 Nivarox-FAR S.A. Silicon-based part with at least one chamfer and method for manufacturing same
WO2017200621A2 (en) 2016-02-29 2017-11-23 The Regents Of The University Of Michigan Assembly processes for three-dimensional microstructures
JP6743619B2 (en) * 2016-09-23 2020-08-19 セイコーエプソン株式会社 Method of manufacturing mechanical part and method of manufacturing timepiece
EP3543795A1 (en) 2018-03-20 2019-09-25 Patek Philippe SA Genève Method for manufacturing silicon clock components

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US640546A (en) * 1898-11-01 1900-01-02 Philo F Dresser Hand-plane.
CH276772A (en) 1948-12-31 1951-07-31 Bulova Watch Co Inc New York S A method of manufacturing anchor wheels for anchor escapements.
US4400861A (en) * 1981-11-27 1983-08-30 Oyo Instruments, Inc. Fabrication of seismic springs from sheets
US5847537A (en) * 1996-10-19 1998-12-08 Parmley, Sr.; Daniel W. Electric vehicle charging station system
JPH1148342A (en) * 1997-08-05 1999-02-23 Sumitomo Heavy Ind Ltd Manufacture of micromachine
DE69904937T2 (en) * 1998-07-03 2003-08-28 Citizen Watch Co Ltd METHOD FOR PRODUCING HANDS FOR ELECTRONIC ANALOG WATCHES
EP0994398B1 (en) * 1998-10-15 2009-01-21 ETA SA Manufacture Horlogère Suisse Method for manufacturing a gear wheel for a timepiece and gear wheel manufactured by said method
DE69917744T2 (en) * 1999-03-05 2005-07-07 Eta Sa Manufacture Horlogère Suisse Dial for watches with diamonds, curbs or other inserted elements and method for attaching these elements to such a dial
EP1139182B1 (en) * 2000-03-27 2007-10-03 Vaucher Manufacture Fleurier SA Reserve power indicating mechanism and timepiece provided with such a mechanism
US6396239B1 (en) * 2001-04-06 2002-05-28 William M. Benn Portable solar generator
US6755225B1 (en) * 2003-01-24 2004-06-29 Quantum Fuel Systems Technologies Worldwide, Inc. Transportable hydrogen refueling station
DE10317889B4 (en) * 2003-04-17 2008-10-30 GFD-Gesellschaft für Diamantprodukte mbH Micromechanical component and method for its production
US7735216B2 (en) * 2004-01-15 2010-06-15 International Business Machines Corporation Micro-electromechanical sub-assembly having an on-chip transfer mechanism
CH699813B1 (en) * 2004-03-25 2010-05-14 Pierre Kunz S A Wheel intended to come into contact with a mobile or fixed element and its manufacturing method.
US7093626B2 (en) * 2004-12-06 2006-08-22 Ovonic Hydrogen Systems, Llc Mobile hydrogen delivery system
SG124309A1 (en) * 2005-01-25 2006-08-30 Sony Corp A material and uses thereof
DE602005025585D1 (en) * 2005-02-23 2011-02-10 Eta Sa Mft Horlogere Suisse Shock absorbing watch storage
CH696475A5 (en) * 2005-05-12 2007-06-29 Eta Sa Mft Horlogere Suisse Body analog display crystalline material, timepiece provided with such a display element and method for its manufacture.
EP1826634A1 (en) * 2006-02-28 2007-08-29 Nivarox-FAR S.A. Micromechanical element provided with form-locking opening for axle assembly
US7721751B1 (en) * 2006-05-09 2010-05-25 Timothy Perrien Fuel dispensing system
EP1921042A1 (en) 2006-11-10 2008-05-14 ETA SA Manufacture Horlogère Suisse Fabrication of multilevel micromechanical silicon components
EP1921520B1 (en) * 2006-11-13 2009-01-28 ETA SA Manufacture Horlogère Suisse Drive module incorporating an MEMS micromotor, manufacturing process for this module, and time piece equipped with this module
US20080190748A1 (en) * 2007-02-13 2008-08-14 Stephen Daley Arthur Power overlay structure for mems devices and method for making power overlay structure for mems devices
EP2268918A2 (en) * 2007-07-27 2011-01-05 Skybuilt Power Renewable energy trailer
US20090187416A1 (en) * 2008-01-17 2009-07-23 Clean Emission Fluids, Inc. Fuel Station Apparatus and Method for Utilizing the Same
JP5300275B2 (en) 2008-01-25 2013-09-25 キヤノン株式会社 Method for manufacturing metal member having a plurality of protrusions
CH699110A1 (en) * 2008-07-10 2010-01-15 Swatch Group Res & Dev Ltd Mechanical component i.e. escape wheel, fabricating method for timepiece, involves assembling attachment on component such that component is ready to be mounted without requiring to touch component, and liberating component from substrate
US8294286B2 (en) * 2008-07-15 2012-10-23 F3 & I2, Llc Network of energy generating modules for transfer of energy outputs
US8295033B2 (en) * 2010-01-21 2012-10-23 George Van Straten Mobile electricity generator using solar, wind, and fuel-generated power
US8899627B2 (en) * 2011-01-13 2014-12-02 Wacker Neuson Production Americas Llc Multiple fuel tank system

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US8661681B2 (en) 2014-03-04
HK1163266A1 (en) 2012-09-07
US20110225801A1 (en) 2011-09-22
EP2359197B1 (en) 2015-01-07
KR20110086579A (en) 2011-07-28
EP2189854A1 (en) 2010-05-26
EP2359197A1 (en) 2011-08-24
JP5548692B2 (en) 2014-07-16
JP2012509197A (en) 2012-04-19
CN102224464A (en) 2011-10-19
TW201029913A (en) 2010-08-16
RU2498382C2 (en) 2013-11-10
WO2010057777A1 (en) 2010-05-27
CN102224464B (en) 2013-04-24
TWI520900B (en) 2016-02-11

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